CN101131094A - 尖端斜面涡轮机叶片 - Google Patents
尖端斜面涡轮机叶片 Download PDFInfo
- Publication number
- CN101131094A CN101131094A CNA2007101417248A CN200710141724A CN101131094A CN 101131094 A CN101131094 A CN 101131094A CN A2007101417248 A CNA2007101417248 A CN A2007101417248A CN 200710141724 A CN200710141724 A CN 200710141724A CN 101131094 A CN101131094 A CN 101131094A
- Authority
- CN
- China
- Prior art keywords
- advanced
- sophisticated
- rib
- afterbody
- fin
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/711—Shape curved convex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410700641.8A CN104594955B (zh) | 2006-08-21 | 2007-08-21 | 尖端斜面涡轮机叶片 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/507,116 US8512003B2 (en) | 2006-08-21 | 2006-08-21 | Tip ramp turbine blade |
US11/507116 | 2006-08-21 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410700641.8A Division CN104594955B (zh) | 2006-08-21 | 2007-08-21 | 尖端斜面涡轮机叶片 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN101131094A true CN101131094A (zh) | 2008-02-27 |
Family
ID=39032230
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410700641.8A Active CN104594955B (zh) | 2006-08-21 | 2007-08-21 | 尖端斜面涡轮机叶片 |
CNA2007101417248A Pending CN101131094A (zh) | 2006-08-21 | 2007-08-21 | 尖端斜面涡轮机叶片 |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410700641.8A Active CN104594955B (zh) | 2006-08-21 | 2007-08-21 | 尖端斜面涡轮机叶片 |
Country Status (5)
Country | Link |
---|---|
US (1) | US8512003B2 (de) |
EP (1) | EP1903183B1 (de) |
JP (1) | JP5306613B2 (de) |
CN (2) | CN104594955B (de) |
CA (1) | CA2597654C (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102042039A (zh) * | 2009-10-21 | 2011-05-04 | 通用电气公司 | 涡轮和涡轮叶片翼片 |
CN102057134A (zh) * | 2008-10-30 | 2011-05-11 | 三菱重工业株式会社 | 具有削薄接片的涡轮动叶片 |
CN103161522A (zh) * | 2011-12-15 | 2013-06-19 | 通用电气公司 | 具有微通道冷却的构件 |
CN106574508A (zh) * | 2014-08-05 | 2017-04-19 | 赛峰飞机发动机公司 | 涡轮机涡轮叶片的凹槽状顶部 |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0724612D0 (en) | 2007-12-19 | 2008-01-30 | Rolls Royce Plc | Rotor blades |
GB0901129D0 (en) | 2009-01-26 | 2009-03-11 | Rolls Royce Plc | Rotor blade |
US8157504B2 (en) * | 2009-04-17 | 2012-04-17 | General Electric Company | Rotor blades for turbine engines |
US8186965B2 (en) * | 2009-05-27 | 2012-05-29 | General Electric Company | Recovery tip turbine blade |
GB201100957D0 (en) * | 2011-01-20 | 2011-03-02 | Rolls Royce Plc | Rotor blade |
US9429027B2 (en) | 2012-04-05 | 2016-08-30 | United Technologies Corporation | Turbine airfoil tip shelf and squealer pocket cooling |
US9004861B2 (en) * | 2012-05-10 | 2015-04-14 | United Technologies Corporation | Blade tip having a recessed area |
US9957817B2 (en) * | 2012-07-03 | 2018-05-01 | United Technologies Corporation | Tip leakage flow directionality control |
US8920124B2 (en) | 2013-02-14 | 2014-12-30 | Siemens Energy, Inc. | Turbine blade with contoured chamfered squealer tip |
GB201406472D0 (en) * | 2014-04-10 | 2014-05-28 | Rolls Royce Plc | Rotor blade |
US20150300180A1 (en) * | 2014-04-22 | 2015-10-22 | United Technologies Corporation | Gas turbine engine turbine blade tip with coated recess |
US10041358B2 (en) * | 2014-05-08 | 2018-08-07 | United Technologies Corporation | Gas turbine engine blade squealer pockets |
US10012089B2 (en) | 2014-05-16 | 2018-07-03 | United Technologies Corporation | Airfoil tip pocket with augmentation features |
CN104196574B (zh) * | 2014-07-15 | 2016-08-24 | 西北工业大学 | 一种燃气涡轮冷却叶片 |
EP3280918B1 (de) | 2015-04-08 | 2021-03-03 | Horton, Inc. | Lüfterschaufel mit druckseitigen durchflussveränderungsmerkmalen |
US10107108B2 (en) | 2015-04-29 | 2018-10-23 | General Electric Company | Rotor blade having a flared tip |
FR3037974B1 (fr) * | 2015-06-29 | 2017-07-21 | Snecma | Procede de fabrication d'une aube comportant une baignoire integrant un muret |
US10677066B2 (en) | 2015-11-23 | 2020-06-09 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
US20170145827A1 (en) * | 2015-11-23 | 2017-05-25 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
US10253637B2 (en) | 2015-12-11 | 2019-04-09 | General Electric Company | Method and system for improving turbine blade performance |
US10830082B2 (en) | 2017-05-10 | 2020-11-10 | General Electric Company | Systems including rotor blade tips and circumferentially grooved shrouds |
US10443405B2 (en) * | 2017-05-10 | 2019-10-15 | General Electric Company | Rotor blade tip |
US20200063571A1 (en) * | 2018-08-27 | 2020-02-27 | Rolls-Royce North American Technologies Inc. | Ceramic matrix composite turbine blade with lightening hole |
US10961854B2 (en) * | 2018-09-12 | 2021-03-30 | Raytheon Technologies Corporation | Dirt funnel squealer purges |
US10801334B2 (en) | 2018-09-12 | 2020-10-13 | Raytheon Technologies Corporation | Cooling arrangement with purge partition |
US11118462B2 (en) * | 2019-01-24 | 2021-09-14 | Pratt & Whitney Canada Corp. | Blade tip pocket rib |
US11136890B1 (en) | 2020-03-25 | 2021-10-05 | General Electric Company | Cooling circuit for a turbomachine component |
CN114109902A (zh) * | 2020-08-25 | 2022-03-01 | 通用电气公司 | 叶片燕尾榫和保持设备 |
US11371359B2 (en) | 2020-11-26 | 2022-06-28 | Pratt & Whitney Canada Corp. | Turbine blade for a gas turbine engine |
US11608746B2 (en) | 2021-01-13 | 2023-03-21 | General Electric Company | Airfoils for gas turbine engines |
Family Cites Families (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3635585A (en) | 1969-12-23 | 1972-01-18 | Westinghouse Electric Corp | Gas-cooled turbine blade |
US3781129A (en) | 1972-09-15 | 1973-12-25 | Gen Motors Corp | Cooled airfoil |
US3854842A (en) * | 1973-04-30 | 1974-12-17 | Gen Electric | Rotor blade having improved tip cap |
US3973874A (en) * | 1974-09-25 | 1976-08-10 | General Electric Company | Impingement baffle collars |
US4010531A (en) | 1975-09-02 | 1977-03-08 | General Electric Company | Tip cap apparatus and method of installation |
US4142824A (en) | 1977-09-02 | 1979-03-06 | General Electric Company | Tip cooling for turbine blades |
US4390320A (en) | 1980-05-01 | 1983-06-28 | General Electric Company | Tip cap for a rotor blade and method of replacement |
US4606701A (en) | 1981-09-02 | 1986-08-19 | Westinghouse Electric Corp. | Tip structure for a cooled turbine rotor blade |
US4424001A (en) | 1981-12-04 | 1984-01-03 | Westinghouse Electric Corp. | Tip structure for cooled turbine rotor blade |
US4497613A (en) * | 1983-01-26 | 1985-02-05 | General Electric Company | Tapered core exit for gas turbine bucket |
US4589823A (en) * | 1984-04-27 | 1986-05-20 | General Electric Company | Rotor blade tip |
US4761116A (en) * | 1987-05-11 | 1988-08-02 | General Electric Company | Turbine blade with tip vent |
US4893987A (en) | 1987-12-08 | 1990-01-16 | General Electric Company | Diffusion-cooled blade tip cap |
US5720431A (en) | 1988-08-24 | 1998-02-24 | United Technologies Corporation | Cooled blades for a gas turbine engine |
GB2227965B (en) | 1988-10-12 | 1993-02-10 | Rolls Royce Plc | Apparatus for drilling a shaped hole in a workpiece |
GB2228540B (en) | 1988-12-07 | 1993-03-31 | Rolls Royce Plc | Cooling of turbine blades |
US5282721A (en) | 1991-09-30 | 1994-02-01 | United Technologies Corporation | Passive clearance system for turbine blades |
US5660523A (en) | 1992-02-03 | 1997-08-26 | General Electric Company | Turbine blade squealer tip peripheral end wall with cooling passage arrangement |
US5261789A (en) | 1992-08-25 | 1993-11-16 | General Electric Company | Tip cooled blade |
US5476364A (en) | 1992-10-27 | 1995-12-19 | United Technologies Corporation | Tip seal and anti-contamination for turbine blades |
JP3416184B2 (ja) * | 1993-02-03 | 2003-06-16 | 三菱重工業株式会社 | ガスタービン空冷動翼の翼先端部の冷却構造 |
US5361828A (en) * | 1993-02-17 | 1994-11-08 | General Electric Company | Scaled heat transfer surface with protruding ramp surface turbulators |
JP3137527B2 (ja) | 1994-04-21 | 2001-02-26 | 三菱重工業株式会社 | ガスタービン動翼チップ冷却装置 |
US5503527A (en) | 1994-12-19 | 1996-04-02 | General Electric Company | Turbine blade having tip slot |
US5738491A (en) * | 1997-01-03 | 1998-04-14 | General Electric Company | Conduction blade tip |
JP3453268B2 (ja) | 1997-03-04 | 2003-10-06 | 三菱重工業株式会社 | ガスタービン翼 |
US6059530A (en) | 1998-12-21 | 2000-05-09 | General Electric Company | Twin rib turbine blade |
US6086328A (en) | 1998-12-21 | 2000-07-11 | General Electric Company | Tapered tip turbine blade |
US6224336B1 (en) * | 1999-06-09 | 2001-05-01 | General Electric Company | Triple tip-rib airfoil |
US6164914A (en) | 1999-08-23 | 2000-12-26 | General Electric Company | Cool tip blade |
US6224337B1 (en) * | 1999-09-17 | 2001-05-01 | General Electric Company | Thermal barrier coated squealer tip cavity |
US6502303B2 (en) * | 2001-05-07 | 2003-01-07 | Chromalloy Gas Turbine Corporation | Method of repairing a turbine blade tip |
US6558119B2 (en) | 2001-05-29 | 2003-05-06 | General Electric Company | Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
US6527514B2 (en) | 2001-06-11 | 2003-03-04 | Alstom (Switzerland) Ltd | Turbine blade with rub tolerant cooling construction |
US6602052B2 (en) * | 2001-06-20 | 2003-08-05 | Alstom (Switzerland) Ltd | Airfoil tip squealer cooling construction |
US6554575B2 (en) * | 2001-09-27 | 2003-04-29 | General Electric Company | Ramped tip shelf blade |
US6672829B1 (en) | 2002-07-16 | 2004-01-06 | General Electric Company | Turbine blade having angled squealer tip |
US6790005B2 (en) | 2002-12-30 | 2004-09-14 | General Electric Company | Compound tip notched blade |
US7270514B2 (en) * | 2004-10-21 | 2007-09-18 | General Electric Company | Turbine blade tip squealer and rebuild method |
US7287959B2 (en) * | 2005-12-05 | 2007-10-30 | General Electric Company | Blunt tip turbine blade |
-
2006
- 2006-08-21 US US11/507,116 patent/US8512003B2/en active Active
-
2007
- 2007-08-06 JP JP2007204372A patent/JP5306613B2/ja not_active Expired - Fee Related
- 2007-08-16 CA CA 2597654 patent/CA2597654C/en active Active
- 2007-08-20 EP EP07114605.4A patent/EP1903183B1/de not_active Ceased
- 2007-08-21 CN CN201410700641.8A patent/CN104594955B/zh active Active
- 2007-08-21 CN CNA2007101417248A patent/CN101131094A/zh active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102057134A (zh) * | 2008-10-30 | 2011-05-11 | 三菱重工业株式会社 | 具有削薄接片的涡轮动叶片 |
CN102057134B (zh) * | 2008-10-30 | 2015-04-22 | 三菱日立电力系统株式会社 | 具有削薄接片的涡轮动叶片 |
CN102042039A (zh) * | 2009-10-21 | 2011-05-04 | 通用电气公司 | 涡轮和涡轮叶片翼片 |
CN102042039B (zh) * | 2009-10-21 | 2016-01-20 | 通用电气公司 | 涡轮和涡轮叶片翼片 |
CN103161522A (zh) * | 2011-12-15 | 2013-06-19 | 通用电气公司 | 具有微通道冷却的构件 |
CN103161522B (zh) * | 2011-12-15 | 2016-07-06 | 通用电气公司 | 具有微通道冷却的构件 |
CN106574508A (zh) * | 2014-08-05 | 2017-04-19 | 赛峰飞机发动机公司 | 涡轮机涡轮叶片的凹槽状顶部 |
Also Published As
Publication number | Publication date |
---|---|
US20080044289A1 (en) | 2008-02-21 |
CN104594955A (zh) | 2015-05-06 |
JP2008051094A (ja) | 2008-03-06 |
CA2597654A1 (en) | 2008-02-21 |
JP5306613B2 (ja) | 2013-10-02 |
CA2597654C (en) | 2015-04-07 |
EP1903183A3 (de) | 2012-05-30 |
CN104594955B (zh) | 2016-11-23 |
US8512003B2 (en) | 2013-08-20 |
EP1903183A2 (de) | 2008-03-26 |
EP1903183B1 (de) | 2017-07-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20080227 |